View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 64216U 26145.40917257 +.00000000 +00000-0 +67074-3 0 00002
2 64216 53.1573 43.1180 0001141 89.2369 270.8762 15.30204762 08
| Epoch (UTC): | 25 May 2026 09:49:12 |
| Eccentricity: | 0.0001141 |
| inclination: | 53.1573° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.1180° |
| argument of perigee: | 89.2369° |
| revolutions per day: | 15.30204762 |
| mean anomaly at epoch: | 270.8762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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